PropulsionSystemDesignLEO:

Path: Propulsion/Demos/Chemical

% Design a propulsion system for a low-earth orbit satellite
We assume a constant orbit for drag purposes. You can add any number
of Hohmann transfers and any number of phase changes. You can add other
maneuvers to this script.
We assume a blowdown system with helium as the pressurant.
The momentum calculations assume a fixed center-of-mass offset.
If one thruster overwhelms the RWA capacity it recommends a 4 thruster
configuration. In that case you use off-pulsing during maneuvers.
See also OrbMnvrHohmann, OrbMnvrPhaseChange, DVOrbitDrag, RocketMass,
BDDesign, Period, Constant, CreateLatexTable, DisplayLatexTable
%